Boeing 727-2Q9

Service difficulty reports · 830

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Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '7272Q9'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DHL2000740005Switch · malfunctionedDURING T/O ROLL LED ANNUNCIATOR LIGHT WENT GREEN THEN AMBER. T/O REJECTED, CHRISTMAS TREE VERIFIED NR 3 FLAP AMBER ABOUT 110 KTS AND 152,800 LBS. REPLACED NR 3 LED FLAP POSITION SWITCH PER M/M 27-82-1. OPS CHK OK.Sep 16, 2000 · N740DH · Boeing 7272Q9 · Leading Edge Slat Position Indicating SystemSDR DHL2000740004Rod End · wornDURING T/O ROLL, LED ANNUNCIATOR WENT FROM GREEN TO AMBER. T/O REJECTED. CHRISTMAS TREE VERIFIED NR 3 FLAP. ABORT 80 KTS AND 152000 LBS. FOUND WORN ROD END ON NR 3 L/E FLAP ACTUATOR. REMOVED AND REPLACED ACTUATOR PER M/M 27-81-22, OPS CHK OK.Sep 16, 2000 · N740DH · Boeing 7272Q9 · Leading Edge Slat ActuatorSDR DHL2000741002Switch · malfunctionedTAKEOFF CONFIGERATION WARNING HORN ACTIVATED DURING INITIAL THRUST APPLICATION. ABORTED TAKEOFF AND TRIED APPLYING POWER AGAIN ON TAXI WAY. HORN SOUNDED AGAIN. REMOVED AND REPLACED FLAP WARNING SWITCH PER M/M 31-26-12. TAKEOFF WARNING SYS TEST COMPLIED WITAug 4, 2000 · N741DH · Boeing 7272Q9 · Trailing Flap Position Indicating SystemSDR DHL2000740003Radome · lightning strikeIP RADAR TILT INOP, 2P TOOK LIGHTNING STRIKE ON RADOME AREA DURING CLIMBOUT. 1P REMOVED AND REPLACED RADAR TRANCEIVER AND RADAR INDR. OPS CHKD OK PER M/M 5-51-171 PG 201. NO DAMAGE FOUND.Jun 13, 2000 · N740DH · Boeing 7272Q9 · Aerodynamic FairingsSDR DHL200074002Line · brokenNR 1 A SYSTEM PUMP LIGHT ILLUMINATED AFTER TAKEOFF, HYD PRESS 3000 PSI, HYD QTY ZERO. SOON AFTER NR 2 PUMP A SYSTEM LIGHT ILLUMINATED AS HYD PRESS DECREASED. FOUND NR 1 PUMP CASE DRAIN LINE BROKEN. REPLACED CASE DRAIN LINE PER MM 29-11-33, REPLACED NR 1 HYDMay 3, 2000 · N740DH · Boeing 7272Q9 · Hydraulic System, MainSDR DHL200074001Trunnion · lack of lubeTWO LOUD BANGS HEARD CLIMBING THRU 12,000 FT 4.5 PSI AND 19,000 FT 5.8 PSI. AFTER FASTENERS REPLACED ON PANEL ABOVE NOSE GEAR TRUNNION AND E & E RACK LUBED PER B727 SERVICE LETTER NOSE GEAR TRUNNION LUBED PER 727 M/M 12-31-11, OPS GOOD PER DHL JRH.Apr 12, 2000 · N740DH · Boeing 7272Q9 · Landing Gear Retraction/Extension SystemSDR DHL2000741001Line · looseON CLIMBOUT, NR 2 ENG SPOOLED BACK TO 1.8 EPR. ATTEMPTED TO GAIN MORE THRUST LEVER MOVEMENT WITH FWD THRUST LEVER MOVEMENT AND ENG FAILED. FOUND LOOSE LINE ON FUEL OIL COOLER TO P&D VLV. ALSO BACK SHELL LOCK WASHER BROKEN AND PACKING CUT. REMOVED AND REPLAMar 30, 2000 · N741DH · Boeing 7272Q9 · Engine Fuel DistributionSDR DHL99740006Switch · failedNR 5 LEADING EDGE FLAP WOULD NOT RETRACT AFTER TAKEOFF. AMBER LIGHT ON FED PANEL DID NOT EXTINGUISH NOR LIGHT ON S/O PANEL. REMOVED AND REPLACED INDICATING SWITCH. OPS CHECKED SYSTEM PER MM 27-82-0.Nov 9, 1999 · N740DH · Boeing 7272Q9 · Leading Edge Slat Position Indicating SystemSDR DHL99740005Retract Mech · malfunctionedWHEN F/O ATTEMPED TO RETRACT GEAR, HANDLE WOULD NOT COME UP PAST NEUTRAL POSITION. PERFORMED CHECKLIST, AT FLAPS 2 WARNING HORN DID NOT SOUND. PULLED GEAR OVERRIDE TRIGGER IN ACCORDANCE WITH CHECK LIST. WITH GEAR HANDLE UP, BOTH YELLOW GEAR WARNING LIGHTS AOct 9, 1999 · N740DH · Boeing 7272Q9 · Landing Gear Retraction/Extension SystemSDR DHL99740004Smoke Detector · failedCARGO SMOKE WARNING LIGHT CAME ON IN FLIGHT AT FL 290. PERFORMED EMERGENCY LANDING AT SDF. REMOVED AND REPLACED SMOKE DETECTOR AMO PER MM 26-13-10.Sep 24, 1999 · N740DH · Boeing 7272Q9 · Smoke DetectionSDR DHL99741004Relay · failedAFTER TAKEOFF, GEAR HANDLE WOULD NOT GO PAST OFF. TAKEOFF WARNING HORN SOUNDED WHEN FLAPS RETRACTED TO 2 DEGREES. CHECKED HANDLE, REMOVED AND REPLACED R92 SAFETY RELAY NAD AIR SENSOR ON LEFT GEAR. CHECKED WIRING AS PER WD 32-31-01. TREATED GEAR HANDLE OPERSep 21, 1999 · N741DH · Boeing 7272Q9 · Landing Gear Position and WarningSDR DHL99740003Smoke Light · looseCARGO SMOKE LIGHT CAME ON IN FLIGHT. DIVERTED TO GEG. INSPECTED ALL SIX SMOKE DETECTOR LIGHTS, FOUND NR 6 BEACON LOOSE. RESECURED BEACON LIGHT, OPS CHECKED GOOD.Sep 14, 1999 · N740DH · Boeing 7272Q9 · Smoke DetectionSDR DHL99740002Valve · failedAFTER DEPARTURE OUT OF PHX, WHEN PLACING GEAR LEVER FROM UP TO OFF, RED PARKING BRAKE ILLUMINATED. SHORTLY THEREAFTER BOTH ANTI SKIN INOP LIGHTS ILLUMINTED. ABOUT 3 MIN LATER FAIL WARNING PARKING BRAKE C/B POPPED. RESET AND POPPED AGAIN. REMOVED AND REPLACJul 22, 1999 · N740DH · Boeing 7272Q9 · Landing Gear Brake SystemSDR DHL99741003Engine · failedAT APPROX 1500 FT NR 2 ENGINE FAILED EGT CLIMBED TO 700 C AND FLIGHT RETURNED TO LAX. REMOVED AND REPLACED ENGINE.Jun 17, 1999 · N741DH · Boeing 7272Q9 · Engine (Turbine/Turboprop)SDR DHL9974134CSeat Track · galledAT C CHECK, NR 2 SEAT TRACK GALLED STA 387. REMOVED SEATTRACK FROM STA 480 TO 600 AND REPLACED PER SRM 53-10-5, N/R 5716.Mar 12, 1999 · N741DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9974121CSkin · delaminatedAT C CHECK, RT WING O/B AFT FLAP T/E DELAMINATED. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8, 10 BY 5, N/R 2898.Mar 6, 1999 · N741DH · Boeing 7272Q9 · Trailing Edge FlapsSDR DHL9974113CSkin · gougedAT C CHECK, INNER SKIN GOUGED AT STA 970 BETWEEN STR 29R AND 28R. CUT OUT DAMAGE, INSTALLED DOUBLER/FILLER PER AVITAS EO 99AVHM001R0-1, FILLER 13.5 BY 3, DOUBLER 25 BY 15.75, N/R 3174.Mar 4, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR DHL9974157CSkin · delaminatedAT C CHECK, LEFT WING I/B FORE FLAP DELAMIANTED IN TWO AREAS AT CENTER SECTION. INSTALLED BONDED REPAIR PER SRM 57-40-6, 10 BY 8 AND 13 BY 17 FT, N/R 1457.Mar 3, 1999 · N741DH · Boeing 7272Q9 · Trailing Edge FlapsSDR DHL9974158CSkin · damagedAT C CHECK, L/T WING I/B MID FLAP LOWER SURFACE LOWER SKIN PANEL HAS A CRACK JUST O/B OF NR 4 TRACK FAIRING. TRIMMED OUT DAMAGED, INSTALLED REPAIR AT LEFT WING MID FLAP PER SRM 57-50-4, 4 BY 22.5, N/R 1452.Mar 2, 1999 · N741DH · Boeing 7272Q9 · Trailing Edge FlapsSDR DHL9974140CFrame · dentedAT C CHECK, FUSELAGE FRAME IS DENTED AT BS 700 ABOVE STRINGER 17R. CUT OUT DAMAGED SECTION. INSTALLED DOUBLER PER SRM 51-40-3, 7 BY 6 FT, N/R 5744.Mar 1, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL9974139CFrame · dentedAT C CHECK, FUSELAGE FRAME DENTED AT BS 720 ABOVE STR 17R. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 51-40-3, 7 BY 4.75, N/R 5745.Mar 1, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL9974124CBob Weight · crackedAT C CHECK, RT ELEVATOR TAB BOB WEIGHT CRACKED AND CORROSION ON CENTER OF O/B BOB WEIGHTS. REMOVED AND REPLACED BOB WEIGHTS PER BOING O/M 55-20-1 AND SRM 51-80-9. N/R 4099Mar 1, 1999 · N741DH · Boeing 7272Q9 · Elevator Control SystemSDR DHL9974117CRib · crackedAT C CHECK, R/W ING NR 8 SLAT, INBD RIB CRACKED. INSTALLED DOUBLER REPAIR PER SRM 57-30-3, 2 BY 6, N/R 2882.Feb 28, 1999 · N741DH · Boeing 7272Q9 · Leading Edge DevicesSDR DHL9974151CFrame · damagedAT C CHECK, FUSELAGE INTERIOR BS 660 IS DAMAGED STR 17R. CUT OUT DAMAGED AREA. INSTALLED DOUBLER PER SRM 51-40-3, 6.5 BY 5.25, N/R 3425.Feb 27, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL9974150CFrame · crackedAT C CHECK, FUSELAGE INTERIOR FRAME BS 640 CRACKED AT STR 17R. CUT OUT DAMAGED AREA, HFEC INSTALLED DOUBLER PER SRM 51-40-3, 7 BY 5 FT, N/R 3426.Feb 27, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL9974149CFrame · crackedAT C CHECK, FUSELAGE INTERIOR FRAME BS 600 HAS CRACK AT STR 17R. CUT OUT DAMAGED AREA. INSTALLED DOUBLER REPAIR PER SRM 51-40-3, 7 BY 5.25, N/R 3427.Feb 27, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL9974148CFrame · crackedAT C CHECK, FUSELAGE INTERIOR FRAME BODY STATION 580 HAS CRACK AT STR 17R. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 51-40-3, 6 BY 4.5, N/R 3428.Feb 27, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL9974147CFrame · crackedAT C CHECK, FUSELAGE INTERIOER FRAME BS 560 HAS CRACK AT STR 17R. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 51-40-3, 7 BY 5.25, N/R 3429.Feb 27, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL9974146CFrame · crackedAT C CHECK, FUSELAGE INTERIOR FRAME BODY STA 540 HAS CRACK AT STR 17R. CUT OUT DAMAGED AREA,HFEC, INSTALLED DOUBLER REPAIR PER SRM 51-40-3, 5.5 BY 6.5, N/R 3430.Feb 27, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL9974144CFrame · damagedAT C CHECK, FUSELAGE FRAME BS 520 IS DAMAGED AT STR 17R. STOP DRILLED AREA, HFEC, INSTALLED DOUBLER PER SRM 51-40-3, 7 BY 6, N/R 3449.Feb 27, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL9974135CStringer · corrodedAT C CHECK, STRINGER 29R HAS CORROSION FROM STA 950 B TO STA 1010. CUT OUT FRAMES AT STA 950F AND 970, CUT OUT DAMAGED SECTION OF STRINGER 29R FROM STA 950D PLUS 8. REMOVED FRAMES AT STA 950D PLUS 5 RT AND 980. INSTALLED REPAIR ON 950 B -950C PER AVITAS EOFeb 27, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR DHL9974112CPlenum · corrodedAT C CHECK, CORROSION ON LEFT AND UPPER WALL OF AIR CONDITIONING PLENUM. INSTALLED SKIN REPAIR PER AVITAS ENGINEERING ORDER 99AVHM 004R0-01, FILLER 19 BY 18, DOUBLER 14 BY 10, TRIPLER 13 BY 9, N/R 3472/3454.Feb 27, 1999 · N741DH · Boeing 7272Q9 · Cabin Cooling SystemSDR DHL9974160CAngle · corrodedAT C-CHECK, FS 307 RBL 12-15 FLANGE OF FLOOR SUPPORT ANGLE DAMAGED AND HAS CORROSION. REMOVED DAMAGED FLOOR SUPPORT, FABRICATED AND INSTALLED NEW SUPPORT PER SRM 53-10-2, 20 X 24.Feb 26, 1999 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL9974152CAngle · corrodedAT C CHECK, INDICATION OF CORROSION AT FWD CARGO COMPARTMENT INTERIOR BS 580 STRINGER 28R RBL 8. REMOVED AND FABRICATED NEW L ANGLE PER SRM 53-10-4, 7 BY 1 BY 1, N/R 3398.Feb 26, 1999 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL9974145CSupport · corrodedAT C CHECK, CORRSOIN ON SUPPORT WEB LOWER END FWD PF 999 CIR O/B OF STR 29R. REMOVED AND REPLACED WEB SUPPORT PER SRM 51-30-2, 4 BY 38, N/R 3437.Feb 26, 1999 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL9974136CSkin · chafedAT C CHECK, INNER FUSELAGE SKIN CHAFFED BY FWD ENTRY DOOR. CUT OUT DAMAGED AREA BETWEEN STR 11L AND 10 L STA 312 PER S/B 53-0198, VISUAL, HFEC AND X-RAY INSPECTED. INSTALLED EXTERNAL DOUBLER REPAIR PER DHLMIA 99-0004RR, 20.5 BY 14.5, N/R 3397/3476.Feb 26, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR DHL9974131CStringer · corrodedAT C CHECK, EVIDENCE OF EXFOLIATION CORROSION AT STRINGER 27R BS 560-567 RBL 14. CUT OUT DAMAGED SECTION AND REPAIRED PER SRM 53-10-3, 12 INCHES LONG, N/R 3396.Feb 26, 1999 · N741DH · Boeing 7272Q9 · Wing, Longeron/StringerSDR DHL9974130CAngle · crackedAT C CHECK, LEFT WING TRAILING EDGE TEMPORARY COVE PANEL SUPPORT ANGLE INSTALLED AT WS 543 CRACKED. REMOVED AND REPLACED ANGLES PER SRM 51-30-2, N/R 1422.Feb 26, 1999 · N741DH · Boeing 7272Q9 · Wing Miscellaneous StructureSDR DHL9974129CAngle · crackedAT C CHECK, LEFT WING FIXED LEADING EDGE CAVITY UPPER OUTBD SUPPORT ANGLE AT SLAT STA 0 IS CRACKED AT AFT ATTACH FASTENERS. REMOVED ANGLE, FABRICATED NEW SUPPORT ANGLE, PER SRM 51-40-3, 16 BY 1.625, N/R 1390.Feb 26, 1999 · N741DH · Boeing 7272Q9 · Wing Miscellaneous StructureSDR DHL9974122CSkin · dentedAT C CHECK, NR 3 SLAT L/E LEADING EDGE EXTERIOR HAS FILLER IN DENT LOCATED 23 FROM OUTBD EDGE. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER 6 BY 9 AND FILLER 2.5 BY 5, PER SRM 57-50-3, N/R 1381.Feb 26, 1999 · N741DH · Boeing 7272Q9 · Leading Edge DevicesSDR DHL9974120CSkin · dentedAT C CHECK, NR 4 SLAT LEADING EDGE EXTEIOR HAS FILLER MATERIAL IN DENT, 16 INCHES FROM OUTBD EDGE. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 57-30-3, 2 BY 2, 6 BY 6, N/R 1383.Feb 26, 1999 · N741DH · Boeing 7272Q9 · Leading Edge DevicesSDR DHL9974115CStringer · corrodedAT C CHECK, CORROSION AT FWD CARGO COMPT BILGE INTERIOER ON STR 27R FS 615 -620 AND 628 RBL 14. CUT OUT DAMAGED SECTION. REPLACED SECTION OF STRINGER FROM 610 TO 630 PER SRM 53-10-3, N/R 3394.Feb 26, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR DHL9974108CSupport · corrodedAT C CHECK, AREA FWD OF E/E COMPARTMENT FS 305 CORROSION ON UNDER SIDE OF FLOOR SUPPORT CHANNEL RBL 0-15. REMOVED FLOOR SUPPORT CHANNEL. FABRICATED ANGLE FLOOR SUPPORT PER SRM 53-10-2, 12 BY 2.5. INSTALLED FLOOR PANELS, N/R 3438.Feb 26, 1999 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL9974107CAngle · crackedAT C CHECK, LEFT WING LEADING EDGE CAVITY INBD MOUNT SUPPORT ANGLE FOR THE NR 2 LEADING EDGE FLAP ACTUATOR IS CRACKED AT THE UPPER CORNER RADIUS. REPLACED MOUNT SUPPORT ANGLE PER SRM 51-30-2, 10 BY 6. REPLACED O/B MOUNT SUPPORT PER SRM 51-30-2, 10 BY 6, N/R Feb 26, 1999 · N741DH · Boeing 7272Q9 · Wing Miscellaneous StructureSDR DHL9974106CSkin · dentedAT C CHECK, NR 1 SLAT LEADING EDGE EXTERIOR HAS FILLER MATERIAL IN DENTS. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 57-30-3, 8 BY 4.5, N/R 1351.Feb 26, 1999 · N741DH · Boeing 7272Q9 · Leading Edge DevicesSDR DHL9974105CFrame · corrodedAT C CHECK, CORROSION AT FRAME AND INTERCOSTAL AT BS 1050 BETWEEN STR 27R AND 28R. REMOVED INTERCOSTAL, FOUND CORROSION ON SKIN, OUT OF LIMITS. REMOVED EXISTING DOUBLER FROM BS 1050 TO 1079. CUT OUT DAMAGED AREA. INSTALLED EXTERNAL SKIN REPAIR PER SRM 53-3Feb 26, 1999 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL9974101CHeat Shield · crackedAT C CHECK, LEFT WING LEADING EDGE INTERIOR ANTI-ICE HEAT SHIELD IS CRACKED AT 3 ATTACH RIVETS. CUT OUT DAMAGED SECTION INSTALLED DOUBLER PER SRM 57-30-4, 13 BY 7, N/R 1440.Feb 26, 1999 · N741DH · Boeing 7272Q9 · Wing Miscellaneous StructureSDR DHL9974159CStrap · chafedAT C CHECK, LEFT WING I/B FORE FLAP DELAMINATED AT I/B END AND CHAFE STRAP BROKEN. INSTALLED FIBERGLASS REPAIR PER SRM 51-40-8, 15 BY 12 FT, N/R 1451.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Trailing Edge FlapsSDR DHL9974155CChannel · crackedAT C CHECK, RT WING LOWER T/E PANEL SUPPORT CHANNEL CRACKED, O/B OF NR 14 SPOILER ACTUATOR STA 601. REMOVED AND REPLACED SUPPORT CHANNEL PER SRM 51-30-2, N/R 2848.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Wing Miscellaneous StructureSDR DHL9974154CChannel · crackedAT C CHECK, RT WING COVE PANEL SUPPORT CHANNEL CRACKED, O/B OF NR 13 SPOILER ACTUATOR STA 500. REMOVED AND REPLACED SUPPORT CHANNEL PER SRM 51-30-2, N/R 2849.Feb 25, 1999 · N741DH · Boeing 7272Q9 · Wing, Plate/Skin
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